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- W2386875296 abstract "Ignition characteristic parameters and affecting factors of small size solid propellant rocket motor is described.The design idea and test situation of aft end ignition for high slenderness ratio,small size solid rocket motors with a tailpipe nozzle are introduced and summerized." @default.
- W2386875296 created "2016-06-24" @default.
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- W2386875296 date "2001-01-01" @default.
- W2386875296 modified "2023-09-25" @default.
- W2386875296 title "Experimental Investigation of Aft End Ignition for High Slenderness Ratio and Small Size Solid Motor" @default.
- W2386875296 hasPublicationYear "2001" @default.
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